Structural frame of a composite material and aircraft...

Details Structural frame of a composite material and aircraft... Structural frame of a composite material and aircraft...

B - Operations, Transporting

29

C

B29C 70/20 (2006.01) B64C 1/06 (2006.01)

Patent

CA 2698617

The invention relates to a structural frame (13) made of a composite material. The purpose of the invention is to obtain a structural frame having high mechanical performance while preserving the simplicity of production. The purpose is achieved by providing assemblies of unidirectional fibres (34) in the main portion (31) of the structural frame at a predetermined angle. The device can be used as a structural frame particularly for an aircraft fuselage.

L'invention concerne un cadre de structure (13) en matériau composite. Le but de l'invention est d'obtenir un cadre de structure présentant des performances mécaniques importantes tout en gardant une simplicité de réalisation. Ce but est atteint en disposant des ensembles de fibres unidirectionnelles (34, 35) dans la partie principale (31) du cadre de structure selon un angle prédéterminé. Ce dispositif peut être utilisé comme cadre de structure notamment pour fuselage d'aéronef.

Affiliated with

Also associated with

Rating

Structural frame of a composite material and aircraft... does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Structural frame of a composite material and aircraft..., we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Structural frame of a composite material and aircraft... will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1479436